Engineering Fundamentals of the Internal Combustion Engine
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A Study of Technology Used and Comparison Between Traditional and Hf120 (Advanced Aero Engine)
International Journal of Recent Technology and Engineering (IJRTE) ISSN: 2277-3878, Volume-4 Issue-4, September 2015 A Study of Technology Used and Comparison Between Traditional and Hf120 (Advanced Aero Engine) Vivek Kumar, Rajeshwar Prasad Singh, Vikash Kumar Abstract- Paper includes detailed study of the HF120 turbofan The two companies began talks in 2003 with the goal of engine, which is the first product from GE Honda Aero providing durable and economical engines for business Engines. This paper is to showcase state of art technology aviation. The idea was to combine the strengths of each involved in gas turbine engines and to bring out various aspects and future trends in field of propulsion technology. parent company in technology leadership, manufacturing Paper also includes development in gas turbine engine that have expertise, and performance engine tradition to provide helped to achieve great fuel efficiency and less noise, increased modern business aviation engines with the performance power, thrust and also advancements made in the field of and availability of large commercial engines. A strategic materials have contributed in a major way in gas turbine in alliance between the two companies lead to planning of accordance to the future trends that have come up in recent 50/50 project intended to develop, certify and market the years. The paper reviews the evolutionary process that has taken place over the years with reference to the different design Honda engine. The HF120, product from GE Honda Aero concepts used for aero engines. At General Electric, the official Engines, utilizes Honda's world-renowned expertise in corporate slogan is “Imagination at work.” At Honda, it’s “The manufacturing, research and development and GE's power of dreams.” Two of the world's most respected names in experience in aerospace technology, durability, and propulsion have come together to design and manufacture certification. -
Methods for Heat Analysis and Temperature Field Analysis of the Insulated Diesel
DOE/NASA/0342-1 NASA CR-174783 19950008390 Methods for Heat Analysis and Temperature Field Analysis of the Insulated Diesel Phase I Progress Report Thomas Morel, Paul N. Blumberg, Edward F. Fort, and Rifat Keribar Integral Technologies Incorporated August 1984 Prepared for NATIONAL AERONAUTICSAND SPACEADMIN ISTRATION Lewis Research Center Under Grant DEN 3-342 1[__ _SPf for ! _i _,:_<,:x._ U.S. DEPARTMENT OF ENERGY L&NGLEY RESEARCHCENTER: Conservationand RenewableEnergy LIBRARYN. ASA Office of Vehicle and Engine R&D .AM__TO_".V,RG,_,_ DISCLAIMER This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof. Printed in the United States of America Available from National Technical Information Service U.S. Department of Commerce 5285 Port Royal Road Springfield, VA 22161 NTIS price codes1 Printed copy: A12 Microfiche copy: A01 1Codes are used for pricing all publications. -
Miniature Free-Piston Homogeneous Charge Compression Ignition Engine
Chemical Engineering Science 57 (2002) 4161–4171 www.elsevier.com/locate/ces Miniature free-piston homogeneous charge compression ignition engine-compressor concept—Part I: performance estimation and design considerations unique to small dimensions H. T. Aichlmayr, D. B. Kittelson, M. R. Zachariah ∗ Departments of Mechanical Engineering and Chemistry, The University of Minnesota, 111 Church St. SE, Minneapolis, MN 55455, USA Received 18 September 2001; received in revised form 7 February 2002; accepted 18 April 2002 Abstract Research and development activities pertaining to the development of a 10 W, homogeneous charge compression ignition free-piston engine-compressor are presented. Emphasis is placed upon the miniature engine concept and design rationale. Also, a crankcase-scavenged, two-stroke engine performance estimation method (slider-crank piston motion) is developed and used to explore the in;uence of engine operating conditions and geometric parameters on power density and establish plausible design conditions. The minimization of small-scale e=ects such as enhanced heat transfer, is also explored. ? 2002 Published by Elsevier Science Ltd. Keywords: Two-stroke engine; Free-piston engine; Homogeneous charge compression ignition; Microchemical; Performance estimation; Micro-power generation 1. Introduction exist: Enhance batteries or develop miniature energy conver- sion devices. Only modest gains may be expected from the This paper is the ÿrst in a two-part series that presents re- former, consequently the latter is being vigorously pursued sults of recent small-scale engine research and development (Peterson, 2001). In particular, miniature engine-generators e=orts conducted at the University of Minnesota. Speciÿ- (Epstein et al., 1997; Yang et al. 1999; Allen et al., 2001; cally, it introduces the miniature free-piston homogeneous Fernandez-Pello, Liepmann, & Pisano, 2001) are considered charge compression ignition (HCCI) engine-compressor especially promising. -
Crankpin Bearings in High Output Aircraft Piston Engines the Evolution of Their Design and Loading by Robert J
Crankpin Bearings in High Output Aircraft Piston Engines The Evolution of their Design and Loading by Robert J. Raymond July 2015 Abstract powered truck. There you will invariably find a 6-cylinder, 4-stroke cycle, open chamber, turbocharged, aftercooled The development of the crankpin bearing in high output engine with electronically controlled fuel injection. Gone are aircraft piston engines is traced over the period 1915-1950 in the two-stroke cycle, divided combustion chambers, and the a large number of liquid and air cooled engines of both many variants of mechanical injection systems found in American and European origin. The changes in bearing truck engines of the past. dimensions are characterized as dimensionless ratios and At the end of the large piston engine era there was still a the resulting changes in the associated weights of rotating broad spectrum of engine configurations being produced and reciprocating parts as weight densities at the crankpin. and actively developed. Along with the major division Bearing materials and developments are presented to indi- between liquid and air-cooled engines there was a turbo- cate how they accommodated increasing bearing loads. compounded engine, a four-row air-cooled radial engine, Bearing loads are characterized by maximum unit bearing engines with poppet valves and engines with sleeve valves, pressure and minimum oil film thickness and plotted as a all in production. There were also a two-stroke turbo-com- function of time. Most of the data was obtained from the lit- pounded Diesel engine, a 2-stroke spark ignition sleeve erature but some results were calculated by the author. -
Heat Engine Driven by Shape Memory Alloys: Prototyping and Design
Heat Engine Driven by Shape Memory Alloys: Prototyping and Design Ean H. Schiller Thesis submitted to the Faculty of Virginia Polytechnic Institute and State University in partial fulfillment of the requirements for a degree of Master of Science in Mechanical Engineering Dr. Charles Reinholtz, Chairman Dr. Harry Robertshaw Dr. Donald J. Leo September 19, 2002 Blacksburg, VA Keywords: shape memory alloy, SMA, Nitinol, heat engine Copyright 2002, Ean Schiller Heat Engine Driven by Shape Memory Alloys: Prototyping and Design Ean H. Schiller (ABSTRACT) This work presents a novel approach to arranging shape memory alloy (SMA) wires into a functional heat engine. Significant contributions include the design itself, a preliminary analytical model and the realization of a research prototype; thereby, laying a foundation from which to base refinements and seek practical applications. Shape memory alloys are metallic materials that, if deformed when cold, can forcefully recover their original, "memorized" shapes, when heated. The proposed engine consists of a set of SMA wires stretched between two crankshafts, synchronized to rotate in the same direction. Cranks on the first crankshaft are slightly longer than cranks on the second. During operation, the engine is positioned between two distinct thermal reservoirs such that half of its wires are heated while the other half are cooled. Wires on the hot side attempt to contract, driving the engine in the direction that relieves the heat-induced stress. Wires on the cold side soften and stretch as the engine rotates. Because the force generated during heated recovery exceeds that required for cooled deformation, the engine is capable of generating shaft power. -
Internal Combustion Engines Collection of Stationary
ASME International THE COOLSPRING POWER MUSEUM COLLECTION OF STATIONARY INTERNAL COMBUSTION ENGINES MECHANICAL ENGINEERING HERITAGE COLLECTION Coolspring Power Museum Coolspring, Pennsylvania June 16, 2001 The Coolspring Power Museu nternal combustion engines revolutionized the world I around the turn of th 20th century in much the same way that steam engines did a century before. One has only to imagine a coal-fired, steam-powered, air- plane to realize how important internal combustion was to the industrialized world. While the early gas engines were more expensive than the equivalent steam engines, they did not require a boiler and were cheap- er to operate. The Coolspring Power Museum collection documents the early history of the internal- combustion revolution. Almost all of the critical components of hundreds of innovations that 1897 Charter today’s engines have their ori- are no longer used). Some of Gas Engine gins in the period represented the engines represent real engi- by the collection (as well as neering progress; others are more the product of inventive minds avoiding previous patents; but all tell a story. There are few duplications in the collection and only a couple of manufacturers are represent- ed by more than one or two examples. The Coolspring Power Museum contains the largest collection of historically signifi- cant, early internal combustion engines in the country, if not the world. With the exception of a few items in the collection that 2 were driven by the engines, m Collection such as compressors, pumps, and generators, and a few steam and hot air engines shown for comparison purposes, the collection contains only internal combustion engines. -
Online Vehicle Database Index 2006 - Issue 3 EXPLANATION VEHICLE TYPE on DATA SHEETS
Online Vehicle Database Index 2006 - Issue 3 EXPLANATION VEHICLE TYPE ON DATA SHEETS 2 Two Seater Man Manual gearbox 4 Four Seater McP McPherson 2+2 Two +Two Seater MPV Multi Purpose Vehicle 2D Two Door MV Mini Van 3D Three Door MWB Middle wheelbase 4D Four Door 5D Five Door NT Narrow track 3HB Three Door Hatchback 5HB Five Door Hatchback O Open 2HT Two Door Hardtop 4HT Four Door Hardtop P Petrol 4L 4-link Suspension PS Power steering 5L 5-link Suspension PU Pick Up 2WD Two Wheel Drive 4WD Four Wheel Drive R Roadster 4WS Four Wheel Steering RC Regular Cab RHD Right Hand Drive Aut Automatic gearbox RWD Rear Wheel Drive AWD All Wheel Drive S3 3 cylinder straight engine B4 4 cylinder Boxer engine S4 4 cylinder straight engine B6 6 cylinder Boxer engine S5 5 cylinder straight engine B Bus S6 6 cylinder straight engine C Coupe S Sedan CO Combi Sh Short CP Compact ShB Short Bed CS Coil Springs Sp Sport CV Convertible/Cab SR Servo CVP Cab Plus Std Standard StdC Standard Cab D Diesel StdV Standard Van SUV Sport Utility Vehicle E Extended SW Station Wagon ExC Extended Cab SWB Short wheelbase ExV Extended Van EV Electric vehicle Ute Utility Vehicle FWD Front Wheel Drive V Van V4 4 cylinder V-engine HB Hatchback V5 5 cylinder V-engine HD Heavy duty V6 6 cylinder V-engine HT Hardtop V8 8 cylinder V-engine V10 10 cylinder V-engine IRS Independent Rear Suspension V12 12 cylinder V-engine LB Liftback W Wankel engine LC Light Commercial WB Wheelbase LHD Left Hand Drive WT Wide track Lo Long LoB Long Bed XLWB Extra long wheelbase LS Leaf Springs LWB Long -
The W Engine Concept
Service. Self-Study Programme 248 The W Engine Concept Design and Function Introduction The constantly rising demands regarding The W engines set exacting demands on design. performance, running comfort and fuel economy Large numbers of cylinders were adapted to the have led to the advancement of existing drive extremely compact dimensions of the engine. units and the development of new drive units. In the process, more attention was paid to lightweight design. The new W8 as well as the W12 engine by This Self-Study Programme will familiarise you VOLKSWAGEN are representatives of a new with the engine mechanicals of the W engine engine generation - the W engines. family. S248_101 New Important Note This Self-Study Programme explains the design Please always refer to the relevant Service Literature for cur- and function of new developments. rent inspection, adjustment and repair instructions. The contents will not be updated! 2 At a glance Introduction . .4 Engine mechanicals . 10 Specifications . 10 The crankshaft drive . .14 The engine in detail . 15 The chain drive . 28 The camshaft timing control . 29 The belt drive . 32 The oil circuit . 34 The coolant circuit . 42 The air supply . 46 The exhaust system . 50 Service . .52 Sealing concept . 52 Engine timing overview. 54 Special tools . 56 3 Introduction W engines - what does the W stand for? With the aim of building even more compact When the W engine is viewed from the front, the units with a large number of cylinders, the design cylinder arrangement looks like a double-V. features of the V and VR engines were combined Put the two Vs of the right and left cylinder banks to produce the W engines. -
Design and Analysis of IC Engine Piston, Piston Rings and Connecting Rod 1 2 3 4 5 6 G
ISSN 2348–2370 Vol.10,Issue.04, April-2018, Pages:0342-0347 www.ijatir.org Design And Analysis of IC Engine Piston, Piston Rings and Connecting Rod 1 2 3 4 5 6 G. MANUSHA , G. KAVYA , K. S. J. SADHANA , NASEER AHMED , SD. INTHIYAZ , T. HARISH BABU Dept of Mechanical Engineering, SVITS, Mahbubnagar, Telangana, India. Abstract: This project mainly deals with the design and expanding gas in the cylinder to the crankshaft via a piston analysis of I.C engine piston, piston rings and connecting rod and/or connecting rod. rod. Piston is a component of reciprocating engines, reciprocating pumps, gas compressors and pneumatic A. Piston cylinders among other similar mechanisms. In an engine, its A piston is a component of reciprocating engines, purpose is to transfer force from expanding gas in the reciprocating pumps, gas compressors and pneumatic cylinder to the crankshaft via a piston rod or connecting rod. cylinders, among other similar mechanisms. For this project, there are two basic requirements. The first requirement is to design of a model of I.C engine piston, piston rings and connecting rod. The second requirement is to analyze of I.C engine piston, piston rings and connecting rod by the method, such as following a track, which consists of straight lines and curves. These systems are done by modeling software’s like CatiaV5, and analysis is done by Ansys software. Specifications of a product are detailed in terms of the product size, speed range, weight and power consumption. Here the piston is designed; analyzed and has been studied. Piston temperature has considerable influence on efficiency, emission, performance of the engine. -
Pyroelectric Energy Harvesting: with Thermodynamic-Based Cycles
Hindawi Publishing Corporation Smart Materials Research Volume 2012, Article ID 160956, 5 pages doi:10.1155/2012/160956 Research Article Pyroelectric Energy Harvesting: With Thermodynamic-Based Cycles Saber Mohammadi and Akram Khodayari Mechanical Engineering Department, School of Engineering, Razi University, Kermanshah 67149-67346, Iran Correspondence should be addressed to Saber Mohammadi, [email protected] Received 30 November 2011; Revised 31 January 2012; Accepted 2 February 2012 Academic Editor: Mickael¨ Lallart Copyright © 2012 S. Mohammadi and A. Khodayari. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. This work deals with energy harvesting from temperature variations using ferroelectric materials as a microgenerator. The previous researches show that direct pyroelectric energy harvesting is not effective, whereas thermodynamic-based cycles give higher energy. Also, at different temperatures some thermodynamic cycles exhibit different behaviours. In this paper pyroelectric energy harvesting using Lenoir and Ericsson thermodynamic cycles has been studied numerically and the two cycles were compared with each other. The material used is the PMN-25 PT single crystal that is a very interesting material in the framework of energy harvesting and sensor applications. 1. Introduction for the systems with limited accessibility such as biomedical implants, structure embedded microsensors, or safety moni- Small, portable, and lightweight power generation systems toring devices. are currently in very high demand in commercial markets, Thermodielectric power generation utilizes the pyroelec- due to a dramatic increase in the use of personal electronics tric effect to convert heat to useful electricity. -
Constant Volume Combustion: the Ultimate Gas Turbine Cycle
INFRASTRUCTURE MINING & METALS NUCLEAR, SECURITY & ENVIRONMENTAL OIL, GAS & CHEMICALS Constant volume combustion: the ultimate gas turbine cycle About Bechtel Bechtel is among the most respected engineering, project management, and construction companies in the world. We stand apart for our ability to get the job done right—no matter how big, how complex, or how remote. Bechtel operates through four global business units that specialize in infrastructure; mining and metals; nuclear, security and environmental; and oil, gas, and chemicals. Since its founding in 1898, Bechtel has worked on more than 25,000 projects in 160 countries on all seven continents. Today, our 58,000 colleagues team with customers, partners, and suppliers on diverse projects in nearly 40 countries. Guest Feature Also in this section Constant volume combustion: 00 DARPA-funded CVC projects the ultimate gas turbine cycle 00 Power cycle thermodynamics 00 History of CVC engineering By S. C. Gülen, PhD, PE; Principal Engineer, Bechtel Power Pulse detonation combustion holds the key to 45% simple cycle and close to 65% combined cycle efficiencies at today’s 1400-1500°C gas turbine firing temperatures. The Kelvin-Planck statement of the Second Law of Thermo- Why constant volume combustion? dynamics leaves no room for doubt: the maximum efficiency In a modern gas turbine with an approximately constant pres- of a heat engine operating in a thermodynamic cycle cannot sure combustor, the compressor section consumes close to exceed the efficiency of a Carnot cycle operating between 50% of gas turbine power output. the same hot and cold temperature reservoirs. Assume one could devise a combustion system where All practical heat engine cycles are attempts to approxi- energy added to the working fluid (i.e. -
Temperature Oscillations in the Wall of a Cooled Multi Pulsejet Propeller For
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Sheffield Hallam University Research Archive Temperature oscillations in the wall of a cooled multi pulsejet propeller for aeronautic propulsion TRANCOSSI, Michele, PASCOA, Jose and CARLOS, Xisto Available from Sheffield Hallam University Research Archive (SHURA) at: http://shura.shu.ac.uk/13964/ This document is the author deposited version. You are advised to consult the publisher's version if you wish to cite from it. Published version TRANCOSSI, Michele, PASCOA, Jose and CARLOS, Xisto (2016). Temperature oscillations in the wall of a cooled multi pulsejet propeller for aeronautic propulsion. SAE Technical Papers, 2016 (1-1998), 1-8. Repository use policy Copyright © and Moral Rights for the papers on this site are retained by the individual authors and/or other copyright owners. Users may download and/or print one copy of any article(s) in SHURA to facilitate their private study or for non- commercial research. You may not engage in further distribution of the material or use it for any profit-making activities or any commercial gain. Sheffield Hallam University Research Archive http://shura.shu.ac.uk Downloaded from SAE International by Michele Trancossi, Monday, November 07, 2016 Temperature Oscillations in the Wall of a Cooled Multi 2016-01-1998 Pulsejet Propeller for Aeronautic Propulsion Published 09/20/2016 Michele Trancossi Shefield Hallam University Jose Pascoa Universidade Da Beira Interior Carlos Xisto Chalmers University of Technology CITATION: Trancossi, M., Pascoa, J., and Xisto , C., "Temperature Oscillations in the Wall of a Cooled Multi Pulsejet Propeller for Aeronautic Propulsion," SAE Technical Paper 2016-01-1998, 2016, doi:10.4271/2016-01-1998.